Microsoft FS2004 Extra 300 S
Flight Dynamic Data Files




Extra300S.air - Datafile : Derivatives

Linear coefficents

In section 1101 Primary Aerodynamics :

Roll, Pitch, Yaw

Lift , Drag

Miscellaneous Data ( no "derivatives" )

Nonlinear coefficients (as correcting factors)

examples:

404 Lift Coeffi vs AoA ,CL_alpha

451 Dihedral Effect Coeff vs Body AoA. Cl_beta_alpha

456 Roll DampingCoeff. vs Bdy AoA, Cl_p

460 Weathervane Stability vs Body AoA , Cn_beta_alpha

464 Yaw Damping Coeff. vs Body AoA ,Cn_r_alpha

473 Pitch Moment Coeff. vs Body AoA Cm_alpha



aircraft.cfg - Data File - Geometry and Masses


examples:

Moments of Inertia